For abstract, see N76-11223.


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    Title :

    An investigation in the NASA MSFC 14-inch trisonic wind tunnel to determine the pressure distribution over the components of a 0.004 scale version of the Rockwell MCR 0074 baseline shuttle ascent configuration (IA32F), volume 3


    Contributors:

    Publication date :

    1975-09-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English